N380NG

No registry detail on file · not in current registry

Operators of this aircraft

Who operated this tail, and how firmly we know it.

No operator established for this aircraft.

Accident & incident history

No NTSB accidents or incidents on file for this aircraft.

Maintenance disclosures

Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.

20 reports on file, 2011-11-29 – 2014-12-30.

OTHER · 2014-12-30 Matched by certificate designator
ATA 5330

Part: SKIN — NICKED (BS 94) · airframe 5,507 hrs · 5,303 cycles

DURING HEAVY CHECK, FOUND SMALL NICK TO ACFT SKIN AT BS 94.800, STR 29R. MX PERFORMED PERMANENT REPAIR IAW RD8/4-53-6617, SKIN, PN 85327051, REF EMERY PO 4591 FOR MATERIAL USED .063, 2024-T3 P/SHEET.

Source: SDR R61A201412300040
OTHER · 2014-12-17 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 5,507 hrs · 5,303 cycles

DURING HEAVY CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK. MAINTENANCE R & R THE SEAT TRACK IAW SRM 51-40-15, 51-41-00, 51-42-05.

Source: SDR R61A201501090023
OTHER · 2014-12-17 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 5,507 hrs · 5,303 cycles

DURING HEAVY CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK. R & R THE SEAT TRACK IAW SRM 51-40-07, 51-40-10, AND 51-42-05.

Source: SDR R61A201501090024
OTHER · 2014-12-15 Matched by certificate designator
ATA 5330

Part: SKIN — DENTED (ZONE 200) · airframe 5,507 hrs · 5,303 cycles

DENTS ON RT FUSELAGE BETWEEN BS 281 - 301 AND STR 16 - 20S. AFT OF ICE SHIELD BELOW WINDOW. MAINTENANCE PERFORMED MAJOR REPAIR IAW RD 8/4-53-6589, ISSUE 1. & SRM 51-42-05 AND 51-40-07.

Source: SDR R61A201412150039
OTHER · 2014-12-15 Matched by certificate designator
ATA 5330

Part: SKIN — DENTED (ZONE 200) · airframe 5,507 hrs · 5,303 cycles

DURING HEAVY CHECK, FUSELAGE SKIN DENTED BY BIRD STRIKES. REPAIRED IAW SRM 51-25-05-02-01, 51-42-05-02-01.

Source: SDR R61A201501280056
OTHER · 2014-11-21 Matched by certificate designator
ATA 5730

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 5,507 hrs · 5,303 cycles

MAINTENANCE FOUND CORROSION ON THE ACCESS PANEL LANDING. MAINTENANCE REPAIRED AREA IAW RD 8/4-57-2694.

Source: SDR R61A201501120026
OTHER · 2014-11-02 Matched by certificate designator
ATA 2560

Part: FLASHLIGHT — MISSING (FWD CABIN) · airframe 5,310 hrs · 5,120 cycles

CREW REPORTED THAT THE FORWARD F/A FLASHLIGHT WAS MISSING. MAINTENANCE INSTALLED A NEW FLASHLIGHT IAW AMM.

Source: SDR R61A201411021147
OTHER · 2014-08-02 Matched by certificate designator
ATA 5210

Part: GUIDE STOP — FAILED (PAX DOOR) · airframe 4,846 hrs · 4,680 cycles

CREW REPORTED THAT THE MAIN CABIN DOOR WOULD NOT OPEN. MAINTENANCE TROUBLESHOT AND FOUND A BAD GUIDE STOP AND CAP. MAINTENANCE R & R GUIDE STOP AND CAP IAW AMM AND OPS CHECKED GOOD.

Source: SDR R61A201408020950
OTHER · 2014-07-21 Matched by certificate designator
ATA 2560

Part: BATTERY — INOPERATIVE (MEGAPHONE) · airframe 4,786 hrs · 4,620 cycles

CREW REPORTED THAT THE MEGAPHONE BATTERY WAS INOPERATIVE. MAINTENANCE R & R THE BATTERY IAW AMM AND OPS CHECKED GOOD.

Source: SDR R61A201407210897
OTHER · 2014-05-14 Matched by certificate designator
ATA 2560

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 4,399 hrs · 4,256 cycles

CREW REPORTED THAT BOTH COCKPIT FLASHLIGHTS WERE INOPERATIVE. MAINTENANCE R & R THE FLASHLIGHTS BATTERIES IAW AMM AND OPS CHECKED GOOD.

Source: SDR R61A201405140648
OTHER · 2014-05-08 Matched by certificate designator
ATA 2560

Part: FLASHLIGHT — MISSING (COCKPIT) · airframe 4,362 hrs · 4,219 cycles

CREW REPORTED THAT BOTH COCKPIT FLASHLIGHTS WERE MISSING.

Source: SDR R61A201405080633
Earlier reports · 2011–2013 · 9 reports

2013

NO TEST · 2013-12-20 Matched by certificate designator
ATA 2560

Part: FLASHLIGHT — INOPERATIVE (ZONE 900) · airframe 3,659 hrs · 3,553 cycles

AFT F/A FLASHLIGHT WAS FOUND TO BE INOPERATIVE. SECURED FLASHLIGHT ENDCAP IAW AMM 25-00-00. OPS CHECKED GOOD.

Source: SDR R61A201312201347
FALSE WARNING · 2013-12-01 Matched by certificate designator
ATA 5270

Part: WARNING LIGHT — FALSE ACTIVATION (CARGO DOOR) · airframe 3,563 hrs · 3,463 cycles

CREW LEVELED OFF AT 11,000 FEET AND RECEIVED "FUSELAGE DOORS" WARNING LIGHT. AFT CARGO DOOR INDICATED RED AND CREW RAN QRH. F/A CALLED COCKPIT AND ADVISED SHE HEARD "BANGING" NOISES FROM THE CARGO BIN AND THAT IT WAS COLD IN THE REAR OF THE PLANE. CREW DECLARED AN EMERGENCY AND RETURNED, LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND BAGGAGE LEANING HARD AGAINST THE CARGO NET. MAINTENANCE PERFORMED OPS CHECK OF THE AFT BAGGAGE DOOR AMM AND NO FAULTS WERE FOUND. AIRCRAFT IS GOOD FOR SERVICE.

Source: SDR R61A201312011268
WARNING INDICATION · 2013-11-20 Matched by certificate designator
ATA 2130

Part: BLOWOUT PANEL — POPPED · airframe 3,509 hrs · 3,412 cycles

CREW STATED THAT THE FUSELAGE DOORS WARNING LIGHT CAME ON DURING ROTATION AND THE ACFT DUMPED PRESSURE. AN EMERGENCY WAS NOT DECLARED AND RETURNED TO LAND WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND AFT BLOW OUT PANEL WAS POPPED. MAINTENANCE SECURRED AFT BLOW OUT PANEL AND PERFORMED A GROUND PRESSURE CHECK IAW AMM. ACFT IS GOOD FOR SERVICE.

Source: SDR R61A201311201227
WARNING INDICATION · 2013-11-19 Matched by certificate designator
ATA 5230

Part: HANDLE — UNSECURE (AFT CARGO DOOR) · airframe 3,504 hrs · 3,406 cycles

CREW RECEIVED FUSELAGE DOOR WARNING LIGHT THAT INDICATED THE AFT CARGO BAY DOOR WAS OPEN. AN EMERGENCY WAS NOT DECLARED, ACFT LOST PRESSURIZATION AT 6000 FT. LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED IAW AMM AND FOUND THE AFT BAGGAGE DOOR HANDLE POPPED OPEN. NO DISCREPANCIES WERE NOTED AND BLOW OUT PLANELS IN AFT CARGO BAY WERE INTACT. ACFT IS GOOD FOR SERVICE.

Source: SDR R61A201311191228
INFLIGHT SEPARATION · 2013-09-20 Matched by certificate designator
ATA 2560

Part: PSU — DISLODGED (CABIN) · airframe 3,151 hrs · 3,059 cycles

CREW REPORTED THAT THE PSU PANEL FELL DOWN AFTER LANDING. MX SECURED PANEL IAW AMM AND OPS CHECKED GOOD. ACFT IS GOOD FOR SERVICE.

Source: SDR R61A201309200893
FLT CONT AFFECTED · 2013-08-09 Matched by certificate designator
ATA 2731

Part: TRIM SYSTEM — MALFUNCTIONED (ZONE 600) · airframe 2,911 hrs · 2,816 cycles

DURING CRUISE, RECEIVED A PITCH TRIM CAUTION LIGHT. AUTOPILOT WAS DISENGAGED AND TRIED TO ACTIVATE THE PITCH TRIM WITH NO SUCCESS. AS ACFT SLOWED DOWN, FORCE NEEDED TO MOVE THE ELEVATORS INCREASED. DECLARED AN EMERGENCY. FLAPS WERE EXTENDED TO 35 AS IT PROVIDED THE MOST CONTROL AND LANDED WITHOUT INCIDENT. OPS CHECKED PITCH TRIM SYS PER AMM AND NO FAULTS FOUND. AS A PRECAUATION, RT ELEVATOR PITCH TRIM ACTUATOR WAS REPLACED THE NEXT NIGHT IAW AMM AND ACFT IS GOOD FOR SERVICE. P

Source: SDR R61A201308090726
WARNING INDICATION · 2013-07-04 Matched by certificate designator
ATA 5230

Part: HANDLE — OUT OF ADJUST (AFT CARGO DOOR) · airframe 2,702 hrs · 2,618 cycles

CREW RECEIVED AN AFT BAGGAGE WARNING LIGHT DURING CLIMB OUT. ACFT PRESSURIZED NORMALLY AND CREW CONTINUED. F/A`S HEARD SOUND OF AFT BAGGAGE DOOR SLAMMING SHUT AROUND 4000 FT ON DESCENT. AN EMERGENCY WAS NOT DECLARED AND ACFT LANDED WITHOUT INCIDENT. MX FOUND THE SILVER BAGGAGE HANDLE WAS POPPED OUT AT THE GATE. MX PERFORMED ADJUSTMENT TEST OF AFT BAGGAGE DOOR IAW AMM AND OPS CHECKED GOOD.

Source: SDR R61A201307040571
WARNING INDICATION · 2013-03-25 Matched by certificate designator
ATA 5270

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 2,184 hrs · 2,108 cycles

WHILE EN ROUTE FROM DEN TO MCI CREW REPORTED THE AFT BAGGAGE DOOR FUSELAGE WARNING LIGHT CAME ON AND THE DOOR SHOWED OPEN ON THE MFD, HOWEVER PRESSURIZATION WAS NORMAL. CREW DID NOT DECLARE AND EMERGENCY AND ELECTED TO RETURN TO DEN WHERE THEY LANDED WITHOUT INCIDENT. DOOR WAS OPEN AND CLOSED BY THE RAMP BEFORE MAINTENANCE COULD CONFIRM POSITION OF THE HANDLE. MAINTENANCE PERFORMED OPS CHECK OF THE DOOR PER BOMBA AMM AND OPS CHECKED GOOD.

Source: SDR R61A201303250306

2011

PARTIAL RPM/PWR LOSS · 2011-11-29 Unresolved
ATA 7200

Part: ENGINE — POWER LOSS (NR 2) · airframe 566 hrs · 532 cycles

DURING INITIAL CLIMB NR 2 ENGINE LOST TORQUE, THEN COMPLETELY LOST POWER. CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD. IN FLIGHT SHUT DOWN.

Source: SDR NSVA2011317